Composite structure having an inorganic coating adhered thereto and method of making same

ABSTRACT

The present disclosure provides a composite structure and associated method for preparing a composite substrate comprising an inorganic coating that is adhered to an organic-based substrate via an adhesion promoting agent comprising a molecule having a urea moiety at one end of the molecule and an alkoxysilane moiety at the other end of the molecule. The use of adhesion promoting agent having at least one of an amine or imine moiety and an alkoxysilane moiety promotes tight adhesion of the inorganic coating to the substrate.

CROSS REFERENCE

This application claims the benefit of U.S. Provisional Application No.61/503,881, filed Jul. 1, 2011, which is incorporated by referenceherein in its entirety.

FIELD

The present disclosure relates generally to composite structures havinginorganic thermal control coatings, and in particular to methods ofpreparing composite structures having an inorganic thermal coating.

BACKGROUND

In recent years, there has been an increasing desire to use compositematerials in various structures. These composites are generallylightweight and therefore provide an opportunity to design lighterstructures that may be useful in vehicles having a longer range,improved fuel efficiency, or a greater payload, depending upon designcriteria.

Composites generally include reinforcing filler encapsulated in a resin.The filler material may be fibers, particulates, woven fabrics, or maybe present in any other appropriate shape and form. The filler materialmay vary, and may include for example carbon fiber, graphite, fiberglass, and other appropriate materials. The resins may include forexample the family of thermoplastic or thermosetting resins such asepoxy, phenolic, and other suitable engineering resins.

Such composites generally may have limited capabilities for controllingthermal exposure. For example, spacecraft, such as satellites anddeep-space craft, are exposed to a wide range of thermal conditionsduring service. A side facing the sun is heated by absorption of directsolar radiation, while a side facing the void of space is cooled byemission of thermal radiation. If the temperature of the structure orpayload becomes too hot or too cold, structural distortion can occurresulting in reduced system capability. Furthermore, payloads such aselectronics, batteries and other critical systems can experience lowerefficiency, non-operation, shortened lifetimes or failures. Thermalcontrol of the spacecraft is therefore important. Various techniqueshave been developed to reduce temperature variations in externalstructural elements such as antennas and booms, and to maintain theinterior of the spacecraft at a temperature suitable for sensitiveequipment, payloads, and occupancy by human beings.

In one thermal control approach, the external surface of the spacecraftis covered with an inorganic thermal coating material. The coating isdesigned to absorb very little solar radiation, yet efficiently radiatethermal energy in the infrared spectrum, thus biasing the overalltemperature of the satellite structure on which it is disposed towardscooler temperatures. The coating is substantially stable to theradiation and low pressure gaseous environment encountered in spacewithout losing its thermal properties by discoloring, darkening, orotherwise degrading over time in the harsh environment of low to highearth orbit. For some applications, the coating also must besufficiently electrically conductive to dissipate electrostatic chargeon the surface of the spacecraft.

Generally, inorganic coating materials have poor adhesion to compositematerials, and have therefore been limited to being applied to aluminumsubstrates. Accordingly, there exists a need to develop improvedcomposite materials and methods of preparing same in which the compositematerial has an inorganic coating adhered to a thermoplastic orthermoset substrate.

BRIEF SUMMARY

The present disclosure is directed to a composite structure andassociated method for preparing a composite substrate that may addressone or more of the aforementioned problems. In one embodiment, thepresent disclosure provides a composite structure comprising aninorganic coating that is adhered to an epoxy-based substrate via anadhesion promoting agent comprising a molecule having a urea moiety atone end of the molecule and an alkoxysilane moiety at the other end ofthe molecule. The use of adhesion promoting agent having a urea moietyand an alkoxysilane moiety promotes tight adhesion of the inorganiccoating to the substrate.

In one embodiment, the adhesion promoting agent may have the followingstructure as shown in formula (I) below:

wherein X is an alkoxy group having from 1 to 3 carbon atoms; andn is a number from 1 to 5.

In some embodiments, the adhesion promoting agent has a structureselected from formulas (II) (1-[3-(trimethoxysilyl)propyl]urea) and(III) (1-[3-(triethoxysilyl)propyl]urea) below:

In addition, the adhesion promoting agent can be present as in formulas(II) and (III), above, or any combination wherein X is a methoxy orethoxy. For example, in some embodiments, the adhesion promoting agentmay comprise a “mixed” molecule having both methoxy and ethoxy moieties.

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING(S)

Having thus described the disclosure in general terms, reference willnow be made to the accompanying drawings, which are not necessarilydrawn to scale, and wherein:

FIG. 1 is a cross-sectional view of a first composite structure inaccordance with an exemplary embodiment of the present disclosure;

FIG. 2 is a is a cross-sectional view of a second composite structure inaccordance with an exemplary embodiment of the present disclosure;

FIG. 3 is a block diagram for a method of preparing a substrate havingan inorganic coating layer adhered thereto.

DETAILED DESCRIPTION

The present disclosure now will be described more fully hereinafter withreference to the accompanying drawings, in which some, but not allembodiments of the disclosure are shown. Indeed, these disclosure may beembodied in many different forms and should not be construed as limitedto the embodiments set forth herein; rather, these embodiments areprovided so that this disclosure will satisfy applicable legalrequirements. Like numbers refer to like elements throughout.

Embodiments of the present disclosure are directed to compositematerials having an inorganic coatings bonded thereto and methods ofpreparing same. With reference to FIG. 1, a composite structure inaccordance with an embodiment of the disclosure is illustrated andbroadly designated by reference numeral 10. Composite structure 10comprises an inorganic coating 14 that is adhered to an epoxyresin-based substrate 12. A layer 16 comprising an adhesion promotingagent is disposed between the inorganic coating 14 and the substrate 12.The adhesion promoting agent comprises an organic molecule having a ureamoiety at one end of the molecule and an alkoxysilane moiety at theother end of the molecule. The inventor of the present disclosure hasfound that the use of an adhesion promoting agent having a urea moietyand an alkoxysilane moiety promotes tight adherence of the inorganiccoating to the substrate.

FIG. 2 illustrates an embodiment of the disclosure in which thesubstrate of the composite structure may comprise any material. In thisembodiment, the composite structure 20 comprises an inorganic coating 14that is adhered to a substrate 22. A layer 16 comprising an adhesionpromoting agent is disposed between the inorganic coating 14 and anepoxy based resin layer 24 that overlies substrate 22. In oneembodiment, the epoxy based resin layer may comprise a paint or similarcoating that has been applied to the surface of the substrate 22.

The inorganic coating may be characterized as being tightly-adhered tothe substrate. Adhesion strength may be tested in accordance with ASTM D3359 Method A. A tape with minimum peel strength 60 oz per inch (astested per ASTM D 3359 Method A), is placed over the a X-scored markingper D 3359 Method A, pressed down and then pulled away abruptly. Theamount of material pulled off with the tape is compared with a standardto rate the adhesion. In these tests, the inorganic coatings testedshowed very little if any removal and qualify as Class 5 of ASTM D 3359Method A; i.e., less than 5% of the inorganic coating is present on thepulled-away tape, and more typically less than 1%. In one embodiment,substantially no inorganic coating is present on the pulled-away tape.

As briefly discussed above, the adhesion promoting agent comprises anorganic molecule having a urea moiety (e.g., H₂N—(CO)—) at one end ofthe molecule and an alkoxysilane moiety at the other end of themolecule. In one embodiment, the adhesion promoting agent comprises amolecule having a silane moiety with a plurality of alkoxy groups at oneend and a urea moiety at the other end. Suitable adhesion promotingagents in accordance with embodiments of the present disclosure may havethe following structure as shown in formula (I) below:

wherein X is an alkoxy group having from 1 to 3 carbon atoms, andn is a number from 1 to 5.

In one embodiment, the adhesion promoting agent has a structure selectedfrom formulas (II) (1-[3-(trimethoxysilyl)propyl]urea) and (III)(1-[3-(triethoxysilyl)propyl]urea) below:

In some embodiments, the adhesion promoting agent can be present as informulas (II) and (III), above, or any combination wherein X is amethoxy or ethoxy. For example, in some embodiments, the adhesionpromoting agent may comprise a “mixed” molecule having both methoxy andethoxy moieties. In further embodiments, the adhesion promoting agentmay include compounds having a silane moiety and more than one urea-likemoiety (e.g., H₂N—(CO)). For example, in some embodiments the adhesionpromoting agent may include a moiety having two or more urea-likefunctional groups. In addition, the adhesion promoting agent may includecompounds in which the alkyl group is attached to two or more urea-likemoieties.

While not wishing to be bound by theory, it is believed that theadhesion promoting agents of formulas (I)-(III) are particularly usefulin bonding of silicate containing inorganic coatings to epoxy-basedmaterials and substrates (collectively referred to herein as simply thesubstrate). In some embodiments, it is theorized that the alkoxymoieties form bonds directly to silicates in the inorganic coating andthe urea moieties form bonds to chemisorbed water in the epoxy basedsubstrate. In particular, it has been observed that it may be desirableto catalyze the adhesion promoting agent with a base (e.g., pH 7+ to 14)to promote bonding between the adhesion promoting agent and the epoxybased substrate. For example, it is theorized that the bonding of theepoxy based substrate to the inorganic coating may occur according tothe following mechanism:

(1) an epoxy resin matrix having chemisorbed water (—OH) on or near thesurface:(−)3C—OH;(2) an adhesion promoting agent (e.g., H₂N—(CO)—NH—(CH₂)₃—SiX₃ having analkoxy groups at one end and a urea moiety (H₂N—(CO)—) at the other endis applied to the surface of the epoxy resin matrix;(3) in the presence of a chemical base (e.g., Off), the urea moietyreacts with the chemisorbed water in the epoxy resin matrix to form acarbon-nitrogen bond “C—N” to the surface of the epoxy based resin:(−)₃C—N—(CO)—NH—(CH₂)₃)—SiX₃+H₂O.Please note that in the above-described mechanism, the reaction betweenthe adhesion promoting agent and the inorganic coating is alsooccurring, but has been left out for simplicity.

In addition, the inventor has also discovered that that above-describedreaction between the epoxy based substrate and the adhesion promotingagent can be improved in some embodiments by exposing thesubstrate/material to water or humid environments prior to applying theadhesion promoting agent to the substrate.

As discussed previously, it has been observed that catalyzing theadhesion promoting agent with a base helps to promote bonding betweenthe adhesion promoting agent and the epoxy based substrate.Advantageously, the inorganic coating itself may serve as the catalystthat initiates bonding between the adhesion promoting agent and theepoxy based substrate. Generally, the inorganic coating is base materialhaving a pH of about 11 or greater. Upon application of the inorganiccoating to the adhesion promoting agent, the inorganic coating catalyzesthe chemical bonding reaction to thereby form a composite structurecomprising an inorganic coating that is adhered to an epoxy-basedsubstrate via the adhesion promoting agent.

Advantageously, the adhesion promoting agents can be used to bond theinorganic coating to the substrate in the absence of treating thesurface of the substrate with an acid or base, such as treatment withhydrofluoric acid, phosphoric acid, sodium hydroxide, lithium hydroxide,and the like.

In addition, it has also been shown that adhesion of the inorganicthermal coating to the substrate can be provided in the absence ofsurface roughness of the substrate. As such, composite structures inaccordance with the disclosure can be provided in which further abrasiontreatment of the substrate is not necessary for adhesion. In fact, ithas been observed that abrasion of the epoxy based substrate/materialmay actually be detrimental to the bonding process. While not wishing tobe bound by theory, it is believed that abrasion (e.g., sanding) mayremove a surface layer and expose underlying components of thesubstrate, such a graphite or carbon fibers, for example, and as aresult, reduce the surface area of the epoxy based substrate/materialthat is available for bonding. In addition, abrasion may also result inremoving a portion of the hydrated surface layer of the epoxy basedsubstrate/material, which would result lower the amount of chemisorbedwater that is available for boding with the adhesion promoting agent.

As discussed above, the presence of chemisorbed water in the epoxy basedsubstrate/material is believed to improve bonding between the adhesionpromoting agent and the epoxy based substrate/material. In someembodiments it may therefore be desirable to first “humidify” thesurface of the epoxy based substrate/material prior to applying theadhesion promoting agent. In some embodiments, the surface of the epoxybased substrate/material may be humidified by exposing the surface towater, mist, a humid atmosphere, and the like.

The selection of the inorganic coating may dependent on the intended useof the composite structure. It should be recognized that a wide varietyof different inorganic coatings may used in various embodiments of thedisclosure. For example, the inorganic coating may include one or moremetallic constituents, metallic oxides, silica-based constituents, andcombinations thereof. In one embodiment, the inorganic coating is silicabased, such as potassium silicate, sodium silicates, and mixturesthereof.

In some embodiments, the inorganic coating is selected so that it has apH greater than 7. For example, in one embodiment, the inorganic coatingcomprises an inorganic pigment (e.g., metal oxide) dispersed in aninorganic binder (e.g., potassium silicate). Potassium silicate as asolution in water is a basic material having a pH that is typicallygreater or equal to about 11. In such an embodiment, the inorganiccoating has a pH that is capable of catalyzing the reaction between theadhesion promoting agent and the epoxy based substrate/material.

In some embodiments, it may be possible to use inorganic coatings havinga pH that is neutral or acidic. In such an embodiment, it may bedesirable to first treat the applied layer of adhesion promoting agentwith a basic material, such as an alkaline substance, in order tocatalyze bonding of the adhesion promoting agent to the substrate. Forexample, the adhesion promoting agent may be catalyzed by blowingammonia vapor over the applied layer of the adhesion promoting agent.

Suitable inorganic coatings that may be used in one or more embodimentsof the disclosure are described in greater detail in U.S. Pat. Nos.5,820,669, 6,099,637, 6,478,259, 6,576,290, and 7,718,227, the contentsof which are hereby incorporated by reference.

The epoxy-based substrate/material may be selected from a wide varietyof epoxy-based substrates/materials. For example, the substrate maycomprise a carbon fiber epoxy matrix composite; glass fiber epoxy matrixcomposite; an epoxy clear coat layer applied to a substrate (e.g.,thermoplastic, thermoset, or other material based substrates); epoxycontaining paints, such as metal filled paints with an epoxy resinmatrix, and the like.

In one embodiment, the disclosure is directed to a composite structurefor use in a spacecraft. In particular, substrates 12, 22 may be anycomponent of a spacecraft, such as, for example, an inflatable component(e.g., a panel, truss, or array), a sun shield (such as for deployablearrays, reflectors, or reconfigurable reflectors), or a thermal blanket.The inorganic coating 14 comprises an inorganic material that isdisposed at an exterior surface of the composite. In embodiments for usein spacecraft, the inorganic material may have a radiation absorptance(α) of less than about 0.2 and an emissivity (ε) of at least about 0.6,and more typically at least about 0.7. As a result, inorganic coating 14is a relatively poor absorber of solar radiation, yet radiates thermalenergy efficiently in the infrared spectrum, thus biasing the overalltemperature of the substrate 14 towards cooler temperatures.

In one embodiment, the adhesion promoting agent can be applied to thesubstrate via rubbing. For example, the adhesion promoting agent may bedispersed in a suitable carrier solvent and then rubbed onto the surfaceof substrate using a suitable cloth or wipe. Suitable solvents mayinclude methanol, ethanol, anhydrous isopropyl alcohol, and the like.Generally, the promoting agent is present in the carrier solvent at aweight percent that is between 1 to 10 weight %, based on the overallweight of the loaded solvent, and in particular, from about 2 to 8weight %, and more particularly at about 5 weight %. Other methods thatmay be used to apply the adhesion promoting agent to the epoxy basedsubstrate/material may include conventional techniques, such as,spraying, brushing, doctor blade coating, and the like, although notnecessarily with equivalent results.

In some embodiments, the inorganic coating is applied as multiple layersonto the surface of the layer of the adhesion promoting agent. In oneembodiment, the inorganic coating is first applied to the layer of theadhesion promoting agent as a “mist coat” (also known as a “fog coat”)in which the inorganic coating is initially applied as a very finecoating. Applying an initial mist coat may 1) help to catalyze thebonding reaction between the adhesion promoting agent and the substrate,as discussed above, and 2) may help reduce running or crawling of theinorganic coating as additional layers are applied. Generally, theinitial mist coat is applied to the layer of the adhesion promotingagent and is allowed to set for about 5 to 15 minutes prior toapplication of a second coat of the inorganic coating.

A useful thickness of the layer of the adhesion promoting agent may befrom about 0.5 microns or greater. In one embodiment, the thickness ofthe layer of the adhesion promoting agent may be greater than any of thefollowing: 0.5 microns, 0.6 microns, 0.7 microns, 0.8 microns, 0.9microns, 1.0 microns, 1.1 microns, 1.2 microns, 1.3 microns, 1.4microns, 1.5 microns, 1.6 microns, 1.7 microns, 1.8 microns, 1.9microns, 2.0 microns, 2.1 microns, 2.2 microns, 2.3 microns, 2.4microns, 2.5 microns, 2.6 microns, 2.7 microns, 2.8 microns, 2.9microns, and 3.0 microns. In other embodiments, the thickness of theadhesion promoting agent may be less than any of the following: 3.5microns, 3.4 microns, 3.3 microns, 3.2 microns, 3.1 microns, 3.0microns, 2.9 microns, 2.8 microns, 2.7 microns, 2.6 microns, 2.5microns, 2.4 microns, 2.3 microns, 2.2 microns, 2.1 microns, 1.9microns, 1.8 microns, 1.7 microns, 1.6 microns, 1.5 microns, 1.4microns, 1.3 microns, 1.2 microns, 1.1 microns, and 1.0 microns.

After the adhesion promoting agent is applied to the substrate it isallowed to dry. Drying may take place at room temperature and undernormal room humidity conditions. Once dried, the inorganic coating isapplied onto the layer of the adhesion promoting agent. The inorganiccoating can be applied using a variety of methods including brushing,spraying, extrusion coating, draw down, and the like. The inorganiccoating is then allowed to dry and cure to form a composite substrate inwhich the inorganic coating is tightly adhered to the substrate.

After drying and/or curing, the inorganic coating layer may be fromabout 0.001 inch to about 0.010 inch thick, and in particular, theinorganic coating layer may be from about 0.001 to about 0.007 inch.

The inorganic coating may be applied as a single coat, or as multiplecoats which are dried between coats. The total thickness of a singlecoat or the total thickness of multiple coats is as set forth above.Even where multiple coats are applied, the inorganic coating is still a“single layer” coating, because its composition is substantiallyhomogeneous throughout all of the coats and between the coats.

The composite structure having an inorganic coating may be used in anythermal control application. In one particular embodiment, it is used astructural member of a spacecraft, such as a communications satellite.

FIG. 3 illustrates an example of an embodiment of a process 100 forapplying an inorganic coating onto an organic-based substrate. Inprocess step 110, an epoxy based substrate is provided. In step 120, thesurface of the substrate is prepped to receive the adhesion promotingagent thereon. This may involve removal of loose dirt, washing with amild detergent to degrease, or other cleaning processes. In general, theparticular cleaning process employed may depend on the chemicalcomposition of the substrate. After surface preparation, the surface ishumidified at step 130. The humidified surface of the substrate is thencoated with a layer of the adhesion promoting agent via rubbing to adesired thickness, in process 140. The layer of the adhesion promotingagent is dried, typically at room temperature and humidity, in process150. During the drying step, the carrier liquid is evaporated to leave alayer of the adhesion promoting agent. The resulting layer of theadhesion promoting agent may have an oily, film-like appearance andfeel. At process step 160, a thin layer of the inorganic coating isapplied as a mist coating onto the substrate overlying the adhesionpromoting agent layer to a desired thickness. The thus applied mistcoating of the inorganic coating layer is then allowed to catalyze thebonding reaction for a desired amount of time at process step 170. Asecond coating of the inorganic coating layer is then applied over themist coat at step 180. The inorganic coating layer is then dried andcured to form a tightly adherent coating on the surface of the substratein process step 190. After a coating of desired thickness has beenapplied, the coated substrate surface may be inspected by any of avariety of techniques in process step 200. Inspection techniques maytest for coating thickness, porosity, bond strength, surface roughness,hardness, etc.

In addition to the exemplary uses described above, the presentdisclosure may also be used in structural concrete applications. Forexample, a composite coating in accordance with the present disclosurecould be used to tightly adhere coated structural members, such asrebar, bolts, screws, and like, to concrete structures. In theseembodiments, the structural members would first be coated with anepoxy-based resin. Prior to being incorporated into a concretestructure, a coating of the adhesion promoting agent would be applied tothe epoxy coated structural member. Thereafter, the coated structuralmember would be added into a wet concrete structure. Since wet concreteis alkaline, it is expected that the wet concrete would catalyze thereaction between the epoxy coating and the adhesion promoting agent toform a tight adhesion between the concrete and the structural member.

EXAMPLES Example 1

A substrate comprising a glass fiber epoxy matrix composite was selectfor testing as a substrate. The substrate was cleaned using anappropriate cleaning technique. The substrate was then rinsed with waterfollowed by rinsing with deionized water. A solution containing 5 wt. %of 1-[3-(trimethoxysilyl)-propyl]urea in reagent grad 2-propanol wasapplied to the surface of the substrate to form a thin layer of thesolution on the substrate. The solution was then allowed to dry at roomtemperature and humidity. The surface of the substrate having a layer ofthe 1-[3-(trimethoxysilyl)-propyl]urea was then coated with an inorganiccoating comprising a potassium silicate. The inorganic coating was thenallowed to dry and cure.

The resulting inorganic coating was tightly adhered to the surface ofthe substrate. The coated substrate was subjected to peel testing inwhich none of the inorganic coating was detected on the pulled-awaytape.

Comparative Example 1

A substrate was prepared and coated with an inorganic coating asdescribed in Example 1 above, with the exception that the substrate wasnot coated with an adhesion promoting agent. Following curing of theinorganic coating, the substrate was subjected to the peel test. Asignificant portion of the coating was present on the pulled-way test.

The process described in Example 1, was also repeated with varioussurface treatments including sanding/roughing of the surface andchemical treatments, such as treatment with basic and acidic substancesprior to applying the adhesion promoting agent or the inorganic coating.The test results showed that adhesion of the inorganic coating to thesubstrate was independent of both mechanical (e.g., sanding/roughening)and chemical (e.g, treatment with acid/basic substances).

Many modifications and other embodiments of the disclosure set forthherein will come to mind to one skilled in the art to which thesedisclosure pertain having the benefit of the teachings presented in theforegoing descriptions and the associated drawings. Therefore, it is tobe understood that the disclosure are not to be limited to the specificembodiments disclosed and that modifications and other embodiments areintended to be included within the scope of the appended claims.Although specific terms are employed herein, they are used in a genericand descriptive sense only and not for purposes of limitation.

That which is claimed:
 1. A composite structure comprising: anepoxy-based matrix, the epoxy-based matrix including chemisorbed water,the chemisorbed water being present by exposing a surface layer of theepoxy-based matrix to water, and wherein the chemisorbed water isdisposed only on the surface layer of the epoxy-based matrix; aninorganic coating layer disposed overlying said surface layer of theepoxy-based matrix having the chemisorbed water; and an adhesionpromoting agent layer disposed between the epoxy-based matrix and theinorganic coating layer, the adhesion promoting agent layer adhering theinorganic coating to the epoxy-based matrix, the adhesion promotingagent having a following formula:

wherein X is an alkoxy group having from 1 to 3 carbon atoms; and n is anumber from 1 to 5, and wherein the inorganic coating layer consists ofone or more of a) potassium silicate, b) sodium silicate, or c) acombination of potassium silicate or sodium silicate with one or more ofa metallic oxide, inorganic pigment, or basic material having a pHgreater than
 7. 2. The composite structure of claim 1, wherein theadhesion promoting agent comprises a molecule having a followingformula:


3. The composite structure of claim 1, wherein the inorganic coatinglayer consists of potassium silicate.
 4. The composite structure ofclaim 1, wherein the epoxy-based matrix comprises glass fibers.
 5. Thecomposite structure of claim 1, wherein the epoxy-based matrix comprisescarbon fibers.
 6. The composite structure of claim 1, wherein theadhesion promoting agent layer has a thickness greater than 0.5 microns.7. The composite structure of claim 1, wherein the epoxy-based matrix iscoated onto a surface of a non-epoxy based material.
 8. The compositestructure of claim 1, wherein the adhesion promoting agent layer has athickness ranging from 0.5 to 3.5 microns.
 9. A concrete compositematerial comprising: a concrete matrix; a structural member disposed inthe concrete matrix, the structural member comprising an epoxy-basedmatrix including chemisorbed water being present by exposing a surfacelayer of the epoxy-based matrix to water, and wherein the chemisorbedwater is disposed only on the surface layer of the epoxy-based matrix,and an adhesion promoting agent adhering the concrete matrix to saidsurface layer of the epoxy-based matrix, wherein the adhesion promotingagent has a following formula:

wherein X is an alkoxy group having from 1 to 3 carbon atoms; and n is anumber from 1 to
 5. 10. The concrete composite material of claim 9,wherein the structural member is rebar.
 11. A composite structurecomprising: an epoxy-based matrix, the epoxy-based matrix havingchemisorbed water, the chemisorbed water being present by exposing asurface layer of the epoxy-based matrix to water, and the chemisorbedwater being disposed only on the surface layer of the epoxy-basedmatrix; an adhesion promoting agent layer overlying said epoxy-basedmatrix, the adhesion promoting agent having a following formula:

wherein X is an alkoxy group having from 1 to 3 carbon atoms; and n is anumber from 1 to 5; and an inorganic coating layer disposed overlyingsaid adhesion promoting agent layer, the inorganic coating layerconsisting of one or more of a) potassium silicate, b) sodium silicate,or c) a combination of potassium silicate or sodium silicate with one ormore of a metallic oxide, inorganic pigment, or basic material having apH greater than 7, and wherein an amount of the inorganic coatingremoved from the epoxy-based substrate is less than 5% when subjected toASTM D 3359 Method A.
 12. The composite structure of claim 11, whereinthe adhesion promoting agent comprises a molecule having a followingformula:


13. The composite structure of claim 11, wherein the inorganic coatinglayer consists of potassium silicate.
 14. The composite structure ofclaim 11, wherein the epoxy-based matrix comprises glass fibers.
 15. Thecomposite structure of claim 11, wherein the epoxy-based matrixcomprises carbon fibers.
 16. The composite structure of claim 11,wherein the adhesion promoting agent layer has a thickness ranging from0.5 to 3.5 microns.
 17. The composite structure of claim 11, wherein theepoxy-based matrix is coated onto a surface of a non-epoxy basedmaterial.
 18. The composite structure of claim 11, wherein the inorganiccoating layer comprises a basic material having a pH greater than
 7. 19.The composite structure of claim 11, wherein an amount of the inorganiccoating removed from the epoxy-based substrate is less than 1% whensubjected to ASTM D 3359 Method A.